Engineering:Kosmos 362

From HandWiki
Kosmos 362
Mission typeABM radar target
COSPAR ID1970-073A
Spacecraft properties
Spacecraft typeDS-P1-I
ManufacturerYuzhnoye
Launch mass300 kilograms (660 lb)
Start of mission
Launch date16 September 1970, 11:59:55 (1970-09-16UTC11:59:55Z) UTC
RocketKosmos-2I 63SM
Launch sitePlesetsk 133/1
End of mission
Decay date13 October 1971 (1971-10-14)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude270 kilometres (170 mi)
Apogee altitude829 kilometres (515 mi)
Inclination71 degrees
Period95.6 minutes
 

Kosmos 362 (Russian: Космос 362 meaning Cosmos 362), also known as DS-P1-I No.9 was a satellite which was used as a radar target for anti-ballistic missile tests. It was launched by the Soviet Union in 1970 as part of the Dnepropetrovsk Sputnik programme.[1]

Launch

It was launched aboard a Kosmos-2I 63SM rocket,[2] from Site 133/1 at Plesetsk. The launch occurred at 11:59:55 UTC on 16 September 1970.[3]

Orbit

Kosmos 362 was placed into a low Earth orbit with a perigee of 270 kilometres (170 mi), an apogee of 829 kilometres (515 mi), 71 degrees of inclination, and an orbital period of 95.6 minutes.[1] It decayed from orbit on 13 October 1971.[4]

Kosmos 362 was the ninth of nineteen DS-P1-I satellites to be launched.[1] Of these, all reached orbit successfully except the seventh.[5]

References

  1. 1.0 1.1 1.2 Wade, Mark. "DS-P1-I". Encyclopedia Astronautica. http://www.astronautix.com/craft/dsp1i.htm. 
  2. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. http://planet4589.org/space/log/launchlog.txt. 
  3. Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. http://www.astronautix.com/lvs/kosmos2.htm. 
  4. McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. http://www.planet4589.org/space/log/satcat.txt. 
  5. Wade, Mark. "DS". Encyclopedia Astronautica. http://www.astronautix.com/project/ds.htm.